Airworthiness Directives; Bombardier, Inc., Airplanes, 87725-87730 [2023-27387]
Download as PDF
87725
Proposed Rules
Federal Register
Vol. 88, No. 242
Tuesday, December 19, 2023
This section of the FEDERAL REGISTER
contains notices to the public of the proposed
issuance of rules and regulations. The
purpose of these notices is to give interested
persons an opportunity to participate in the
rule making prior to the adoption of the final
rules.
DEPARTMENT OF AGRICULTURE
Food and Nutrition Service
7 CFR Parts 271 and 275
[FNS–2020–0016]
RIN 0584–AE79
Provisions To Improve the
Supplemental Nutrition Assistance
Program’s Quality Control System
Food and Nutrition Service
(FNS), USDA.
ACTION: Proposed rule; reopening of
comment period.
AGENCY:
The U.S. Department of
Agriculture proposed to make changes
to the Supplemental Nutrition
Assistance Program’s Quality Control
(SNAP QC) system to strengthen and
improve the integrity and accuracy of
the system and to better align SNAP QC
with requirements in the Payment
Integrity Information Act of 2019 (PIIA).
When published, the proposed rule
included an incorrect email address for
comments; the reopening of the
comment period is intended to allow
additional time for the public to submit
comments in the event the original
comment submission was returned as
undeliverable due to the incorrect email
address.
DATES: The comment period for the
proposed rule published September 19,
2023, at 88 FR 64756, is reopened.
Written comments must be received on
or before January 2, 2024 to ensure their
consideration.
ADDRESSES: The Food and Nutrition
Service, USDA, invites interested
persons to submit written comments on
this proposed rule. Comments may be
submitted in writing by one of the
following methods:
—Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow
the online instructions for submitting
comments.
—Mail: Send comments to John
McCleskey, Branch Chief, Quality
lotter on DSK11XQN23PROD with PROPOSALS1
SUMMARY:
VerDate Sep<11>2014
17:04 Dec 18, 2023
Jkt 262001
Control Branch, Program
Accountability and Administration
Division; Food and Nutrition Service,
1320 Braddock Place, 5th Floor,
Alexandria, Virginia 22314.
—E-Mail: Send comments to
SM.FN.SNAPQCReform@usda.gov.
Include Docket ID Number FNS–
2020–0016, ‘‘Provisions to Improve
the SNAP QC System’’ in the subject
line of the message.
—All written comments submitted in
response to this proposed rule will be
included in the record and will be
made available to the public. Please
be advised that the substance of the
comments and the identity of the
individuals or entities submitting the
comments will be subject to public
disclosure. FNS will make the written
comments publicly available on the
internet via https://
www.regulations.gov.
John
McCleskey, 703–457–7747, Food and
Nutrition Service, 1320 Braddock Place,
5th Floor, Alexandria, Virginia 22314,
SM.FN.SNAPQCReform@usda.gov.
FOR FURTHER INFORMATION CONTACT:
In a notice
of proposed rulemaking, published on
September 19, 2023 (88 FR 64756), the
email address provided in the addresses
section of the rule was incorrect,
resulting in comments submitted via
email being returned as undeliverable.
While the other avenues for comment
submission were unaffected, USDA is
correcting the email address and
allowing the public additional time to
submit comments. Commenters who do
not see their comment reflected on
www.regulations.gov from the original
comment period are encouraged to
resubmit their comments. All regulatory
provisions in the September 19, 2023,
proposed rule remain unchanged. This
document notifies the public the
Department is reopening the comment
period until January 2, 2024.
SUPPLEMENTARY INFORMATION:
Cynthia Long,
Administrator, Food and Nutrition Service.
[FR Doc. 2023–27821 Filed 12–18–23; 8:45 am]
BILLING CODE 3410–30–P
PO 00000
Frm 00001
Fmt 4702
Sfmt 4702
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–2242; Project
Identifier MCAI–2023–00704–T]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc., Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain Bombardier, Inc., Model BD–
100–1A10 airplanes. This proposed AD
was prompted by a determination that
new or more restrictive maintenance
tasks are necessary. This proposed AD
would require revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive maintenance tasks. The FAA
is proposing this AD to address the
unsafe condition on these products.
DATES: The FAA must receive comments
on this proposed AD by February 2,
2024.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
regulations.gov. Follow the instructions
for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–2242; or in person at
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this NPRM, the mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The street address for
Docket Operations is listed above.
Material Incorporated by Reference:
SUMMARY:
E:\FR\FM\19DEP1.SGM
19DEP1
87726
Federal Register / Vol. 88, No. 242 / Tuesday, December 19, 2023 / Proposed Rules
• For service information identified
in this NPRM, contact Bombardier
Business Aircraft Customer Response
Center, 400 Coˆte-Vertu Road West,
Dorval, Que´bec H4S 1Y9, Canada;
telephone 514–855–2999; email ac.yul@
aero.bombardier.com; website
bombardier.com.
• You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA,
call 206–231–3195.
FOR FURTHER INFORMATION CONTACT:
Gabriel Kim, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–
228–7300; email 9-avs-nyaco-cos@
faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2023–2242; Project Identifier
MCAI–2023–00704–T’’ at the beginning
of your comments. The most helpful
comments reference a specific portion of
the proposal, explain the reason for any
recommended change, and include
supporting data. The FAA will consider
all comments received by the closing
date and may amend the proposal
because of those comments.
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to
regulations.gov, including any personal
information you provide. The agency
will also post a report summarizing each
substantive verbal contact received
about this NPRM.
lotter on DSK11XQN23PROD with PROPOSALS1
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this NPRM
contain commercial or financial
information that is customarily treated
as private, that you actually treat as
private, and that is relevant or
responsive to this NPRM, it is important
that you clearly designate the submitted
comments as CBI. Please mark each
page of your submission containing CBI
as ‘‘PROPIN.’’ The FAA will treat such
VerDate Sep<11>2014
17:04 Dec 18, 2023
Jkt 262001
marked submissions as confidential
under the FOIA, and they will not be
placed in the public docket of this
NPRM. Submissions containing CBI
should be sent to Gabriel Kim, Aviation
Safety Engineer, FAA, 1600 Stewart
Avenue, Suite 410, Westbury, NY
11590; telephone 516–228–7300; email
9-avs-nyaco-cos@faa.gov. Any
commentary that the FAA receives
which is not specifically designated as
CBI will be placed in the public docket
for this rulemaking.
Background
Transport Canada, which is the
aviation authority for Canada, has
issued Transport Canada AD CF–2023–
34, dated May 25, 2023 (Transport
Canada AD CF–2023–34) (also referred
to after this as the MCAI), to correct an
unsafe condition for all Bombardier,
Inc., Model BD–100–1A10 airplanes.
The MCAI states that new or more
restrictive maintenance tasks have been
developed.
Airplanes with certain serial numbers
were delivered after the maintenance or
inspection program was revised and
must comply with the airworthiness
limitations specified as part of the
approved type design and referenced on
the type certificate data sheet; this
proposed AD therefore does not include
those airplanes in the applicability.
The FAA is proposing this AD to
address failure or degradation of the
horizontal stabilizer trim actuator
(HSTA) and motor brake assembly. A
failed or degraded HSTA or motor brake
assembly could result in loss of control
of the airplane. You may examine the
MCAI in the AD docket at
regulations.gov under Docket No. FAA–
2023–2242.
Related Service Information Under 1
CFR Part 51
The FAA reviewed the following
Bombardier service information, which
describes new or more restrictive
airworthiness limitation maintenance
tasks that specify inspection and
overhaul of the HSTA and add flightcycle and flight-hour limitations.
• Sections 5–10–20, ‘‘Time Limits—
Supplementary Limitations,’’ and 5–10–
40, ‘‘Certification Maintenance
Requirements,’’ of part 2,
‘‘Airworthiness Limitations,’’ of the
Bombardier Challenger 350 Time
Limits/Maintenance Check, CH 350,
Revision 13, dated June 14, 2022, which
include Task 27–40–00–104*,
‘‘Restoration (Overhaul) of the
Horizontal-Stabilizer Trim-Actuator
(HSTA), Part No. C47100–004 and
subs,’’ and Task 27–41–05–104*,
‘‘Restoration (Overhaul) of the
PO 00000
Frm 00002
Fmt 4702
Sfmt 4702
Horizontal-Stabilizer Trim-Actuator
(HSTA), Part No. C47100–004/–005.’’
• Sections 5–10–20, ‘‘Time Limits—
Supplementary Limitations,’’ and 5–10–
40, ‘‘Certification Maintenance
Requirements,’’ of part 2,
‘‘Airworthiness Limitations,’’ of the
Bombardier Challenger 300 Time
Limits/Maintenance Check, CH 300,
Revision 23, dated June 14, 2022, which
include Task 27–40–00–104*,
‘‘Restoration (Overhaul) of the
Horizontal-Stabilizer Trim-Actuator
(HSTA), Part No. C47100–004 and
subs,’’ and Task 27–41–05–104*,
‘‘Restoration (Overhaul) of the
Horizontal-Stabilizer Trim-Actuator
(HSTA), Part No. C47100–004/–005.’’
• Temporary Revision 5–2–31, dated
January 31, 2023, which includes Task
27–40–00–108**, ‘‘Restoration
(Inspection) of the Horizontal-Stabilizer
Trim-Actuator (HSTA), Part No.
C47100–003 and subs.’’
• Temporary Revision 5–2–102, dated
January 31, 2023, which includes Task
27–40–00–108**, ‘‘Restoration
(Inspection) of the Horizontal-Stabilizer
Trim-Actuator (HSTA), Part No.
C47100–003 and subs.’’
These documents are distinct since
they apply to different airplane models.
This service information is reasonably
available because the interested parties
have access to it through their normal
course of business or by the means
identified in ADDRESSES.
FAA’s Determination
This product has been approved by
the aviation authority of another
country and is approved for operation in
the United States. Pursuant to the FAA’s
bilateral agreement with this State of
Design Authority, the FAA has been
notified of the unsafe condition
described in the MCAI and service
information referenced above. The FAA
is proposing this AD because the FAA
evaluated all the relevant information
and determined the unsafe condition
described previously is likely to exist or
develop on other products of the same
type design.
Proposed Requirements of This NPRM
This proposed AD would require
revising the existing maintenance or
inspection program, as applicable, to
incorporate new or more restrictive
maintenance tasks.
This proposed AD would require
revisions to certain operator
maintenance documents to add new
actions (i.e., inspections) and certain
overhaul time limitations. Compliance
with these actions is required by 14 CFR
91.403(c). For airplanes that have been
previously modified, altered, or repaired
E:\FR\FM\19DEP1.SGM
19DEP1
Federal Register / Vol. 88, No. 242 / Tuesday, December 19, 2023 / Proposed Rules
in the areas addressed by this proposed
AD, the operator may not be able to
accomplish the actions described in the
revisions. In this situation, to comply
with 14 CFR 91.403(c), the operator
must request approval for an alternative
method of compliance according to
paragraph (i)(1) of this proposed AD.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 737
airplanes of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD:
The FAA has determined that revising
the maintenance or inspection program
takes an average of 90 work-hours per
operator, although the agency
recognizes that this number may vary
from operator to operator. Since
operators incorporate maintenance or
inspection program changes for their
affected fleet(s), the FAA has
determined that a per-operator estimate
is more accurate than a per-airplane
estimate. Therefore, the agency
estimates the average total cost per
operator to be $7,650 (90 work-hours ×
$85 per work-hour).
lotter on DSK11XQN23PROD with PROPOSALS1
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
The FAA is issuing this rulemaking
under the authority described in
Subtitle VII, Part A, Subpart III, Section
44701: General requirements. Under
that section, Congress charges the FAA
with promoting safe flight of civil
aircraft in air commerce by prescribing
regulations for practices, methods, and
procedures the Administrator finds
necessary for safety in air commerce.
This regulation is within the scope of
that authority because it addresses an
VerDate Sep<11>2014
17:04 Dec 18, 2023
Jkt 262001
unsafe condition that is likely to exist or
develop on products identified in this
rulemaking action.
Regulatory Findings
The FAA determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would not
have a substantial direct effect on the
States, on the relationship between the
national Government and the States, or
on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify this proposed regulation:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Would not affect intrastate
aviation in Alaska, and
(3) Would not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
Bombardier, Inc.: Docket No. FAA–2023–
2242; Project Identifier MCAI–2023–
00704–T.
PO 00000
Frm 00003
Fmt 4702
Sfmt 4702
87727
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by February 1,
2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc.,
Model BD–100–1A10 airplanes, certificated
in any category, having serial numbers 20003
through 20500 inclusive, and 20501 through
20959 inclusive.
(d) Subject
Air Transport Association (ATA) of
America Code 05, Time Limits/Maintenance
Checks; 27, Stabilizer.
(e) Reason
This AD was prompted by a determination
that new or more restrictive maintenance
tasks are necessary. The FAA is issuing this
AD to address failure or degradation of the
horizontal stabilizer trim actuator (HSTA)
and motor brake assembly. The unsafe
condition, if not addressed, could result in
loss of control of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Maintenance or Inspection Program
Revision
Within 60 days after the effective date of
this AD, revise the existing maintenance or
inspection program, as applicable, to
incorporate the information specified in
figure 1 or 2 to paragraph (g) of this AD, as
applicable. The initial compliance time for
doing the tasks is at the time specified in the
applicable temporary revision (TR) or time
limit/maintenance check (TLMC) document
specified in figures 1 and 2 to paragraph (g)
of this AD, or within 60 days after the
effective date of this AD, whichever occurs
later.
Note 1 to paragraph (g): The asterisk (or
‘‘one star’’) or double asterisk (‘‘two star’’)
with the last three digits of the task numbers
listed in figures 1 and 2 to paragraph (g) of
this AD indicates that the task is an
airworthiness limitation task.
BILLING CODE 4910–13–P
E:\FR\FM\19DEP1.SGM
19DEP1
87728
Federal Register / Vol. 88, No. 242 / Tuesday, December 19, 2023 / Proposed Rules
Figure 1 to paragraph (g) - Tasks for Model BD-100-lAlO airplanes
VerDate Sep<11>2014
Task number
Task title
TLMC
chapter
TLMC or TR document
27-40-00-108**
Restoration
(Inspection) of
the HorizontalStabilizer TrimActuator (HSTA),
Part No. C47100003 and subs
5-10-40
Bombardier Temporary
Revision 5-2-102, dated
January 31, 2023
27-40-00-104*
Restoration
(Overhaul) of the
HorizontalStabilizer TrimActuator (HSTA),
Part No. C47100004 and subs
5-10-40
Part 2, "Airworthiness
Limitations," of the
Bombardier Challenger
300 Time
Limits/Maintenance
Check, CH 300, Revision
23, dated June 14, 2022
27-41-05-104*
Restoration
(Overhaul) of the
Horizontal
Stabilizer Trim
actuator (HSTA),
Part No. C47100004/-005
5-10-20
Part 2, "Airworthiness
Limitations," of the
Bombardier Challenger
300 Time
Limits/Maintenance
Check, CH 300, Revision
23, dated June 14, 2022
17:04 Dec 18, 2023
Jkt 262001
PO 00000
Frm 00004
Fmt 4702
Sfmt 4725
E:\FR\FM\19DEP1.SGM
19DEP1
EP19DE23.018
lotter on DSK11XQN23PROD with PROPOSALS1
having SIN s 20003 through 20500
Federal Register / Vol. 88, No. 242 / Tuesday, December 19, 2023 / Proposed Rules
87729
Figure 2 to paragraph (g) - Tasks for Model BD-100- lAlO airplanes having SIN s
20501 through 20959
Task number
Task title
TLMC chapter
TLMC or TR document
27-40-00-108**
Restoration
(Inspection) of
the HorizontalStabilizer
Trim-Actuator
(HSTA), Part
No. C47100003 and subs
5-10-40
Bombardier Temporary
Revision 5-2-31, dated
January 31, 2023
27-40-00-104*
Restoration
(Overhaul) of
the HorizontalStabilizer
Trim-Actuator
(HSTA), Part
No. C47100004 and subs
5-10-40
Part 2, "Airworthiness
Limitations," of the
Bombardier Challenger
350 Time
Limits/Maintenance
Check, CH 350, Revision
13, dated June 14, 2022
27-41-05-104*
Restoration
(Overhaul) of
the Horizontal
Stabilizer Trim
5-10-20
actuator
(HSTA), Part
No. C47100004/-005
Part 2, "Airworthiness
Limitations," of the
Bombardier Challenger
350 Time
Limits/Maintenance
Check, CH 350, Revision
13, dated June 14, 2022
(h) No Alternative Actions, or Intervals
lotter on DSK11XQN23PROD with PROPOSALS1
After the existing maintenance or
inspection program has been revised as
required by paragraph (g) of this AD, no
alternative actions (e.g., inspections) or
intervals may be used unless the actions and
intervals are approved as an alternative
method of compliance (AMOC) in
accordance with the procedures specified in
paragraph (i)(1) of this AD.
(i) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Validation Branch, FAA, has the authority to
approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19.
In accordance with 14 CFR 39.19, send your
request to your principal inspector or
responsible Flight Standards Office, as
appropriate. If sending information directly
to the manager of the International Validation
VerDate Sep<11>2014
17:04 Dec 18, 2023
Jkt 262001
Branch, mail it to ATTN: Program Manager,
Continuing Operational Safety, at the address
identified in paragraph (j)(2) of this AD or
email to: 9-avs-nyaco-cos@faa.gov. If mailing
information, also submit information by
email. Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, International Validation
Branch, FAA; or Transport Canada; or
Bombardier Inc.’s Transport Canada Design
Approval Organization (DAO). If approved by
the DAO, the approval must include the
DAO-authorized signature.
(j) Additional Information
(1) Refer to Transport Canada AD CF–
2023–34, dated May 25, 2023, for related
information. This Transport Canada AD may
be found in the AD docket at regulations.gov
under Docket No. FAA–2023–2242.
PO 00000
Frm 00005
Fmt 4702
Sfmt 4702
(2) For more information about this AD,
contact Gabriel Kim, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516–
228–7300; email 9-avs-nyaco-cos@faa.gov.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) Section 5–10–20, ‘‘Time Limits—
Supplementary Limitations,’’ of Part 2,
‘‘Airworthiness Limitations,’’ of the
Bombardier Challenger 300 Time Limits/
Maintenance Check, CH 300, Revision 23,
dated June 14, 2022.
(ii) Section 5–10–20, ‘‘Time Limits—
Supplementary Limitations,’’ of Part 2,
‘‘Airworthiness Limitations,’’ of the
Bombardier Time Limits/Maintenance Check,
CH 350, Revision 13, dated June 14, 2022.
E:\FR\FM\19DEP1.SGM
19DEP1
EP19DE23.019
BILLING CODE 4910–13–C
87730
Federal Register / Vol. 88, No. 242 / Tuesday, December 19, 2023 / Proposed Rules
(iii) Section 5–10–40, ‘‘Certification
Maintenance Requirements,’’ of Part 2,
‘‘Airworthiness Limitations,’’ of the
Bombardier Challenger 300 Time Limits/
Maintenance Check, CH 300, Revision 23,
dated June 14, 2022.
(iv) Section 5–10–40, ‘‘Certification
Maintenance Requirements,’’ of Part 2,
‘‘Airworthiness Limitations,’’ of the
Bombardier Time Limits/Maintenance Check,
CH 350, Revision 13, dated June 14, 2022.
(v) Bombardier Temporary Revision 5–2–
31, dated January 31, 2023.
(vi) Bombardier Temporary Revision 5–2–
102, dated January 31, 2023.
(3) For service information identified in
this AD, contact Bombardier Business
Aircraft Customer Response Center, 400 CoˆteVertu Road West, Dorval, Que´bec H4S 1Y9,
Canada; telephone 514–855–2999; email
ac.yul@aero.bombardier.com; website
bombardier.com.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th
St., Des Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(5) You may view this material at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
visit www.archives.gov/federal-register/cfr/
ibr-locations or email fr.inspection@nara.gov.
Issued on December 8, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–27387 Filed 12–18–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2023–2429; Airspace
Docket No. 23–AGL–37]
RIN 2120–AA66
Amendment of Class D and Class E
Airspace; Anderson, IN
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
This action proposes to
amend the Class D and Class E airspace
at Anderson, IN. The FAA is proposing
this action as the result of an airspace
review conducted due to the
decommissioning of the Muncie very
high frequency omnidirectional range
(VOR) as part of the VOR Minimum
Operating Network (MON) Program. The
name of the airport would also be
updated to coincide with the FAA’s
aeronautical database. This action will
lotter on DSK11XQN23PROD with PROPOSALS1
SUMMARY:
VerDate Sep<11>2014
17:04 Dec 18, 2023
Jkt 262001
bring the airspace into compliance with
FAA orders to support instrument flight
rule (IFR) operations.
DATES: Comments must be received on
or before February 2, 2024.
ADDRESSES: Send comments identified
by FAA Docket No. FAA–2023–2429
and Airspace Docket No. 23–AGL–37
using any of the following methods:
* Federal eRulemaking Portal: Go to
www.regulations.gov and follow the
online instruction for sending your
comments electronically.
* Mail: Send comments to Docket
Operations, M–30; U.S. Department of
Transportation, 1200 New Jersey
Avenue SE, Room W12–140, West
Building Ground Floor, Washington, DC
20590–0001.
* Hand Delivery or Courier: Take
comments to Docket Operations in
Room W12–140 OF THE West Building
Ground Floor at 1200 New Jersey
Avenue SE, Washington, DC, between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays.
* Fax: Fax comments to Docket
Operations at (202) 493–2251.
Docket: Background documents or
comments received may be read at
www.regulations.gov at any time.
Follow the online instructions for
accessing the docket or go to Docket
Operations in Room W12–140 of the
West Building Ground Floor at 1200
New Jersey Avenue SE, Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
FAA Order JO 7400.11H, Airspace
Designations and Reporting Points, and
subsequent amendments can be viewed
online at www.faa.gov/air_traffic/
publications/. You may also contact the
Rules and Regulations Group, Office of
Policy, Federal Aviation
Administration, 800 Independence
Avenue SW, Washington, DC 20591;
telephone: (202) 267–8783.
FOR FURTHER INFORMATION CONTACT:
Jeffrey Claypool, Federal Aviation
Administration, Operations Support
Group, Central Service Center, 10101
Hillwood Parkway, Fort Worth, TX
76177; telephone (817) 222–5711.
SUPPLEMENTARY INFORMATION:
section, the FAA is charged with
prescribing regulations to assign the use
of airspace necessary to ensure the
safety of aircraft and the efficient use of
airspace. This regulation is within the
scope of that authority as it would
amend the Class D airspace and the
Class E airspace extending upward from
700 feet above the surface at Anderson
Municipal Airport-Darlington Field,
Anderson, IN, to support IFR operations
at this airport.
Authority for This Rulemaking
Comments Invited
The FAA invites interested persons to
participate in this rulemaking by
submitting written comments, data, or
views. Comments are specifically
invited on the overall regulatory,
aeronautical, economic, environmental,
and energy-related aspects of the
proposal. The most helpful comments
reference a specific portion of the
proposal, explain the reason for any
recommended change, and include
supporting data. To ensure the docket
does not contain duplicate comments,
commenters should submit only one
time if comments are filed
electronically, or commenters should
send only one copy of written
comments if comments are filed in
writing.
The FAA will file in the docket all
comments it receives, as well as a report
summarizing each substantive public
contact with FAA personnel concerning
this proposed rulemaking. Before acting
on this proposal, the FAA will consider
all comments it received on or before
the closing date for comments. The FAA
will consider comments filed after the
comment period has closed if it is
possible to do so without incurring
expense or dely. The FAA may change
this proposal in light of the comments
it receives.
Privacy: In accordance with 5 U.S.C.
553(c), DOT solicits comments from the
public to better inform its rulemaking
process. DOT post these comments,
without edit, including any personal
information the commenter provides, to
www.regulations.gov as described in the
system of records notice (DOT/ALL–
14FDMS), which can be reviewed at
www.dot.gov/privacy.
The FAA’s authority to issue rules
regarding aviation safety is found in
Title 49 of the United States Code.
Subtitle I, Section 106 describes the
authority of the FAA Administrator.
Subtitle VII, Aviation Programs,
describes in more detail the scope of the
agency’s authority. This rulemaking is
promulgated under the authority
described in Subtitle VII, Part A,
Subpart I, Section 40103. Under that
Availability of Rulemaking Documents
An electronic copy of this document
may be downloaded through the
internet at www.regulations.gov.
Recently published rulemaking
documents can also be accessed through
the FAA’s web page at www.faa.gov/air_
traffic/publications/airspace_
amendments/.
You may review the public docket
containing the proposal, any comments
PO 00000
Frm 00006
Fmt 4702
Sfmt 4702
E:\FR\FM\19DEP1.SGM
19DEP1
Agencies
[Federal Register Volume 88, Number 242 (Tuesday, December 19, 2023)]
[Proposed Rules]
[Pages 87725-87730]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-27387]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-2242; Project Identifier MCAI-2023-00704-T]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier, Inc., Model BD-100-1A10 airplanes. This
proposed AD was prompted by a determination that new or more
restrictive maintenance tasks are necessary. This proposed AD would
require revising the existing maintenance or inspection program, as
applicable, to incorporate new or more restrictive maintenance tasks.
The FAA is proposing this AD to address the unsafe condition on these
products.
DATES: The FAA must receive comments on this proposed AD by February 2,
2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-2242; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this NPRM, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
street address for Docket Operations is listed above.
Material Incorporated by Reference:
[[Page 87726]]
For service information identified in this NPRM, contact
Bombardier Business Aircraft Customer Response Center, 400 C[ocirc]te-
Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada; telephone 514-
855-2999; email bombardier.com">ac.yul@aero.bombardier.com; website bombardier.com.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195.
FOR FURTHER INFORMATION CONTACT: Gabriel Kim, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-
228-7300; email [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2023-2242; Project Identifier
MCAI-2023-00704-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
the proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to
Gabriel Kim, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516-228-7300; email [email protected]. Any commentary that the FAA receives which is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.
Background
Transport Canada, which is the aviation authority for Canada, has
issued Transport Canada AD CF-2023-34, dated May 25, 2023 (Transport
Canada AD CF-2023-34) (also referred to after this as the MCAI), to
correct an unsafe condition for all Bombardier, Inc., Model BD-100-1A10
airplanes. The MCAI states that new or more restrictive maintenance
tasks have been developed.
Airplanes with certain serial numbers were delivered after the
maintenance or inspection program was revised and must comply with the
airworthiness limitations specified as part of the approved type design
and referenced on the type certificate data sheet; this proposed AD
therefore does not include those airplanes in the applicability.
The FAA is proposing this AD to address failure or degradation of
the horizontal stabilizer trim actuator (HSTA) and motor brake
assembly. A failed or degraded HSTA or motor brake assembly could
result in loss of control of the airplane. You may examine the MCAI in
the AD docket at regulations.gov under Docket No. FAA-2023-2242.
Related Service Information Under 1 CFR Part 51
The FAA reviewed the following Bombardier service information,
which describes new or more restrictive airworthiness limitation
maintenance tasks that specify inspection and overhaul of the HSTA and
add flight-cycle and flight-hour limitations.
Sections 5-10-20, ``Time Limits--Supplementary
Limitations,'' and 5-10-40, ``Certification Maintenance Requirements,''
of part 2, ``Airworthiness Limitations,'' of the Bombardier Challenger
350 Time Limits/Maintenance Check, CH 350, Revision 13, dated June 14,
2022, which include Task 27-40-00-104*, ``Restoration (Overhaul) of the
Horizontal-Stabilizer Trim-Actuator (HSTA), Part No. C47100-004 and
subs,'' and Task 27-41-05-104*, ``Restoration (Overhaul) of the
Horizontal-Stabilizer Trim-Actuator (HSTA), Part No. C47100-004/-005.''
Sections 5-10-20, ``Time Limits--Supplementary
Limitations,'' and 5-10-40, ``Certification Maintenance Requirements,''
of part 2, ``Airworthiness Limitations,'' of the Bombardier Challenger
300 Time Limits/Maintenance Check, CH 300, Revision 23, dated June 14,
2022, which include Task 27-40-00-104*, ``Restoration (Overhaul) of the
Horizontal-Stabilizer Trim-Actuator (HSTA), Part No. C47100-004 and
subs,'' and Task 27-41-05-104*, ``Restoration (Overhaul) of the
Horizontal-Stabilizer Trim-Actuator (HSTA), Part No. C47100-004/-005.''
Temporary Revision 5-2-31, dated January 31, 2023, which
includes Task 27-40-00-108**, ``Restoration (Inspection) of the
Horizontal-Stabilizer Trim-Actuator (HSTA), Part No. C47100-003 and
subs.''
Temporary Revision 5-2-102, dated January 31, 2023, which
includes Task 27-40-00-108**, ``Restoration (Inspection) of the
Horizontal-Stabilizer Trim-Actuator (HSTA), Part No. C47100-003 and
subs.''
These documents are distinct since they apply to different airplane
models.
This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in ADDRESSES.
FAA's Determination
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, the
FAA has been notified of the unsafe condition described in the MCAI and
service information referenced above. The FAA is proposing this AD
because the FAA evaluated all the relevant information and determined
the unsafe condition described previously is likely to exist or develop
on other products of the same type design.
Proposed Requirements of This NPRM
This proposed AD would require revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive maintenance tasks.
This proposed AD would require revisions to certain operator
maintenance documents to add new actions (i.e., inspections) and
certain overhaul time limitations. Compliance with these actions is
required by 14 CFR 91.403(c). For airplanes that have been previously
modified, altered, or repaired
[[Page 87727]]
in the areas addressed by this proposed AD, the operator may not be
able to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must request
approval for an alternative method of compliance according to paragraph
(i)(1) of this proposed AD.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 737 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
The FAA has determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although the
agency recognizes that this number may vary from operator to operator.
Since operators incorporate maintenance or inspection program changes
for their affected fleet(s), the FAA has determined that a per-operator
estimate is more accurate than a per-airplane estimate. Therefore, the
agency estimates the average total cost per operator to be $7,650 (90
work-hours x $85 per work-hour).
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
Bombardier, Inc.: Docket No. FAA-2023-2242; Project Identifier MCAI-
2023-00704-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by February 1, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-100-1A10
airplanes, certificated in any category, having serial numbers 20003
through 20500 inclusive, and 20501 through 20959 inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks; 27, Stabilizer.
(e) Reason
This AD was prompted by a determination that new or more
restrictive maintenance tasks are necessary. The FAA is issuing this
AD to address failure or degradation of the horizontal stabilizer
trim actuator (HSTA) and motor brake assembly. The unsafe condition,
if not addressed, could result in loss of control of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Maintenance or Inspection Program Revision
Within 60 days after the effective date of this AD, revise the
existing maintenance or inspection program, as applicable, to
incorporate the information specified in figure 1 or 2 to paragraph
(g) of this AD, as applicable. The initial compliance time for doing
the tasks is at the time specified in the applicable temporary
revision (TR) or time limit/maintenance check (TLMC) document
specified in figures 1 and 2 to paragraph (g) of this AD, or within
60 days after the effective date of this AD, whichever occurs later.
Note 1 to paragraph (g): The asterisk (or ``one star'') or
double asterisk (``two star'') with the last three digits of the
task numbers listed in figures 1 and 2 to paragraph (g) of this AD
indicates that the task is an airworthiness limitation task.
BILLING CODE 4910-13-P
[[Page 87728]]
[GRAPHIC] [TIFF OMITTED] TP19DE23.018
[[Page 87729]]
[GRAPHIC] [TIFF OMITTED] TP19DE23.019
BILLING CODE 4910-13-C
(h) No Alternative Actions, or Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) or intervals may be used unless the
actions and intervals are approved as an alternative method of
compliance (AMOC) in accordance with the procedures specified in
paragraph (i)(1) of this AD.
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Validation Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the procedures found in 14 CFR
39.19. In accordance with 14 CFR 39.19, send your request to your
principal inspector or responsible Flight Standards Office, as
appropriate. If sending information directly to the manager of the
International Validation Branch, mail it to ATTN: Program Manager,
Continuing Operational Safety, at the address identified in
paragraph (j)(2) of this AD or email to: [email protected]. If
mailing information, also submit information by email. Before using
any approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector, the manager of the responsible Flight
Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Validation Branch, FAA; or Transport Canada; or Bombardier Inc.'s
Transport Canada Design Approval Organization (DAO). If approved by
the DAO, the approval must include the DAO-authorized signature.
(j) Additional Information
(1) Refer to Transport Canada AD CF-2023-34, dated May 25, 2023,
for related information. This Transport Canada AD may be found in
the AD docket at regulations.gov under Docket No. FAA-2023-2242.
(2) For more information about this AD, contact Gabriel Kim,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; email [email protected].
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Section 5-10-20, ``Time Limits--Supplementary Limitations,''
of Part 2, ``Airworthiness Limitations,'' of the Bombardier
Challenger 300 Time Limits/Maintenance Check, CH 300, Revision 23,
dated June 14, 2022.
(ii) Section 5-10-20, ``Time Limits--Supplementary
Limitations,'' of Part 2, ``Airworthiness Limitations,'' of the
Bombardier Time Limits/Maintenance Check, CH 350, Revision 13, dated
June 14, 2022.
[[Page 87730]]
(iii) Section 5-10-40, ``Certification Maintenance
Requirements,'' of Part 2, ``Airworthiness Limitations,'' of the
Bombardier Challenger 300 Time Limits/Maintenance Check, CH 300,
Revision 23, dated June 14, 2022.
(iv) Section 5-10-40, ``Certification Maintenance
Requirements,'' of Part 2, ``Airworthiness Limitations,'' of the
Bombardier Time Limits/Maintenance Check, CH 350, Revision 13, dated
June 14, 2022.
(v) Bombardier Temporary Revision 5-2-31, dated January 31,
2023.
(vi) Bombardier Temporary Revision 5-2-102, dated January 31,
2023.
(3) For service information identified in this AD, contact
Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 514-855-2999; email bombardier.com">ac.yul@aero.bombardier.com; website
bombardier.com.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
(5) You may view this material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Issued on December 8, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-27387 Filed 12-18-23; 8:45 am]
BILLING CODE 4910-13-P